Supersonic wind tunnelsNozzle design codes developed earlier were modified and used in order to design asupersonic wind tunnel nozzle with square cross-sections. As part of the design process, a post-processing code that generates square nozzles from the output of the Sivells code was written. ...
A small-scale supersonic wind tunnel can represent a convenient platform for supersonic flow testing. The scale considered in this work, with maximum cross-sectional area of 1”x1”, requires simpler structure in addition to the low budget costs and minor space requirements. While the small size...
A supersonic wind tunnel, currently in existence at ·the University of Central Florida in Orlando, Florida, is examined to determine feasibility for conversion to a ,vind tunnel with hypersonic capability. Computational data are presented, and the determination is made that the existing wind tunnel...
A method for designing wind tunnel models of conceptual, low-boom, supersonic cruise aircraft is presented. Also included is a review of the procedures used to design the conceptual low-boom aircraft. In the discussion, problems unique to, and encountered during, the design of both the conceptu...
A design method was developed to specify the profile of the continuously variable Mach-number nozzle for the supersonic wind tunnel. The controllable contour design technique was applied to obtaining the original nozzle profile, while other Mach-numbers were derived from the transformation of the orig...
12.Mach Number Seven and Eight Nozzle Design of the Diameter One Meter Hypersonic Wind Tunnel and Flow Field Testing;Φ1米高超声速风洞M7、8喷管设计及流场校测 13.Research of Second Throat Design of Continuous Transonic/Supersonic Wind Tunnel连续式跨声速风洞第二喉道设计技术研究 14.The System of ...
Supersonic travel Supersonic travel Supersonic Tunnel Association International Supersonic Wave Drive supersonic waves Supersonic wind tunnel Supersonic Winds of Neptune Supersonic/Hypersonic Vehicle Supersonic/Hypersonic Vehicle - Design Simulation System Supersonic/Hypersonic Vehicle Design supersonically supe...
Design of a Multipurpose Wind Tunnel A continuously operating wind tunnel was designed for light scattering experiments in supersonic two‐phase flow. Special features permit easy modification... Stein,D Gilbert - 《Review of Scientific Instruments》 被引量: 13发表: 1969年 Wind tunnel experimental ...
Some aspects concerning the design of flexible nozzles for use in supersonic wind tunnels are discussed. Methods are investigated for matching the deflection patterns of nozzle plates and the theoretical aerodynamic shapes required for uniform, parallel, shockfree flow. Application of the design procedu...
The high-load compressor plays an important role in further improving the performance of aero-engine. However, the complex shock waves in the cascade channel also bring more aerodynamic losses. This paper proposes a supersonic compressor cascade modeling method based on the theory of unique inlet ...